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- Видео 59
- Просмотров 29 033
Rafat Alnoty
Добавлен 3 фев 2014
Видео
Fuselage configuration layout and loft
Просмотров 1293 года назад
Fuselage configuration layout and loft
Floating Objects ,Buoyancy Force and Sink Rate.
Просмотров 423 года назад
Floating Objects ,Buoyancy Force and Sink Rate.
Pressure Measurements (Manometer and Bourdon Tube)
Просмотров 323 года назад
Pressure Measurements (Manometer and Bourdon Tube)
Unsymmetrical Bending (Aircraft Structure)
Просмотров 733 года назад
Unsymmetrical Bending (Aircraft Structure)
O Beam Pure Bending (Aircraft Structure)
Просмотров 203 года назад
O Beam Pure Bending (Aircraft Structure)
O Beam Pure Torsion (Aircraft Structure)
Просмотров 313 года назад
O Beam Pure Torsion (Aircraft Structure)
Pure bending I beam (Aircraft Structure)1
Просмотров 323 года назад
Pure bending I beam (Aircraft Structure)1
Unsymmetrical Bending Theories (Arabic)
Просмотров 133 года назад
Unsymmetrical Bending Theories (Arabic)
Thermodynamic Cycles PV and TS Diagrams
Просмотров 423 года назад
Thermodynamic Cycles PV and TS Diagrams
Aircraft Design Workshop 17th of Sep2020
Просмотров 2013 года назад
Aircraft Design Workshop 17th of Sep2020
Just a plain good video. So simple can it be. All the relevant info in a very short video. I like it...
what is control parameter, why you took its value from 0 to 1
Best video I've seen so far thank you
so proud to see this knowledge comes from arab country !!! appreciate it a lot thanks man
Why did you put a 2 kg mass in the point -10m (instead of -0.010 m). Thats changes Cm and the whole calculations and makes them false
I have a problem with the cp location in xflr5.On condition that the angle of attack increases, the cp location will come to near the front side of the wing, but in my program, the cp location does not come to the front side of the wing on the contrary my cp location goes backward.
I have a problem with the cp location in xflr5.On condition that the angle of attack increases, the cp location will come to near the front side of the wing, but in my program, the cp location does not come to the front side of the wing on the contrary my cp location goes backward.
Hello, can you say do we have a calculation for the center of pressure? How can I calculate the place of the pressure center with my hand?
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this? Like which parameters should I consider for generating the view of root locus graph. It would be a huge favour if u could help me out
While doing stability analysis on xflr5 I'm facing some errors that's why the modes for longitudinal and lateral stability are not operating could you plz guide me through this?
Thanks rafat
Hello, can you please upload the XML file for the fuse? I can't find it at all. Please upload it on a public drive or share it file hosting service.
How much the cost of this setup??
How can get this
Sourceforge; "Xflr5"
السلام عليكم استاذ ممكن الايميل للتواصل او رقمً الواتساب
In The explanation of How do Airplanes fly or how lift is produced the theory of one flows over the upper surface and the other lower and meeting at TE is wrong
Hi, is it possible to get the handouts?
Transfer theory is wrong......although many people think this to be true
16 girls interested in aerospace engineering, wow. In my university there are 5 girls and 65 boys
great explaination sir!
Great video! Please enable youtube auto subtitles
Great video! Please enable youtube auto subtitles
thank you!! it helped in my project.
Good job 👍🏻
السلام عليكم اخوي احتاج اكلمك وين اقدر اتواصل معاك ؟
Ralnouti@hct.ac.ae
Very good "هندسة "
Very useful tips. Thank you.
Thanks for the informative video. The adjustment of flow speed is a clever way to avoid the hassle of changing the airfoil coordinates.